Abstract:

The present invention provides an apparatus and a method for producing a
large-area fibre-composite structural component, in particular for the
aircraft sector, comprising a predetermined shaping element, a
controllable laying device for the defined laying of at least one fibrous
sheet over or into the predetermined shaping element, a controllable
turning device for a defined turning of the predetermined shaping element
and of the laying device in relation to each other by a predetermined
turning angle, and a central control device, which is connected to the
laying device and the turning device for controlling of the same.

Claims:

1. Apparatus for producing a large-area fibre-composite structural
component, in particular for the aircraft sector, comprising:a
predetermined shaping element;a controllable laying device for the
defined laying of at least one fibrous sheet over or into the
predetermined shaping element, the laying device having four
synchronously controllable lifting columns, which are arranged in pairs
around the shaping element, each pair of lifting columns being
respectively assigned a vertically adjustable cross member, wherein in
each cross member there are respectively integrated two receiving
carriages for receiving predetermined fibrous sheet rolls that can be
displaced synchronously along the respective cross member;a controllable
turning device for a defined turning of the predetermined shaping element
and of the laying device in relation to each other by a predetermined
turning angle; anda central control device, which is connected to the
laying device and the turning device for controlling of the same.

2. Apparatus according to claim 1, wherein the predetermined shaping
element has approximately the form of a turned-out, shallow dish.

3. Apparatus according to claim 1, wherein the predetermined shaping
element has an oval or circular cross section.

4. Apparatus according to claim 1, wherein the predetermined shaping
element is formed suitably for the forming of a pressure dome of an
aircraft.

5. Apparatus according to claim 1, wherein the receiving carriages have an
electronic drive device each that can be controlled by the central
control device synchronously with the other receiving carriages.

6. Apparatus according to claim 1, wherein the central control device is
connected to the lifting columns for a synchronous vertical adjustment of
the assigned cross members along the longitudinal direction of the
lifting columns and to the receiving carriages for a synchronous
transverse adjustment of the receiving carriages along the cross members.

7. Apparatus according to claim 1, wherein the laying device has a
transfer device for receiving the fibrous sheet, rolled up on two fibrous
sheet rolls, from a transporting car in a defined transfer position.

8. Apparatus according to claim 1, wherein the turning device has a
controllable turntable for receiving and positioning the predetermined
shaping element in relation to the laying device.

9. Apparatus according to claim 8, wherein the turntable has an electronic
drive device that can be controlled by the central control device.

10. Apparatus according to claim 1, wherein the apparatus has an
adjustable podium for access to any region of the shaping element by a
member of the operating personnel.

11. Apparatus according to claim 10, wherein the podium is adjustable
along a rail system and has at least one pivotable platform.

12. Apparatus according to claim 1, wherein the apparatus has a
positioning device, for example a marking device, a linear laser
projector system or the like, for positioning the fibrous sheet to be
laid and/or any additional reinforcing means in conjunction with the
defined position of the turning device.

13. Apparatus according to claim 1, wherein the apparatus has in the
event of failure of the automatic control by means of the central control
device an emergency operating device for a manual emergency mode to
perform the defined laying of the fibrous sheet.

14. Method for producing a large-area fibre-composite structural
component, in particular for the aircraft sector, comprising:providing of
a predetermined shaping element;advance rolling up of a fibrous sheet to
be laid on two fibrous sheet rolls, which are received by means of a
controllable laying device;defined laying of the fibrous sheet over or
into the predetermined shaping element by adjusting the two fibrous sheet
rolls both in the vertical direction and in the transverse direction and
guiding the two fibrous sheet rolls uniformly and synchronously from the
centre of the predetermined shaping element to the edge of the same by
means of the controllable laying device;turning of the predetermined
shaping element and the controllable laying device in relation to each
other by a predetermined turning angle by means of a controllable turning
device; anddefined laying of a further fibrous sheet on top of the
already laid fibrous sheet by means of the controllable laying device.

15. Method according to claim 14, wherein the laying device and the
turning device are controlled by a central control device.

16. Method according to claim 14, wherein a number of fibrous sheets, for
example six, are laid one on top of the other over or into the
predetermined shaping element, after each laying of a fibrous sheet the
predetermined shaping element being turned by means of the turning device
by a predetermined turning angle, by for example 30.degree., in relation
to the laying device and arrested.

17. Method according to claim 14, wherein the two fibrous sheet rolls are
guided in a self-supporting manner approximately 50 mm above the
predetermined shaping element.

18. Method according to claim 14, wherein a predetermined unrolling rate,
a predetermined advancing rate and/or a predetermined advancing amount of
the fibrous sheet to be laid are controlled by the central control device
during the laying of the same over or into the shaping element.

19. Method according to claim 14, wherein, in the event of failure of the
automatic control by means of the central control device, the laying
device is operated in an emergency mode for manual laying of the fibrous
sheet.

Description:

FIELD OF INVENTION

[0001]The present invention relates to an apparatus and a method for
producing a large-area fibre-composite structural component, in
particular for the aircraft sector.

BACKGROUND OF THE INVENTION

[0002]Although it can be applied to any desired large-area fibre-composite
structural components, the present invention and the problem on which it
is based are explained in more detail with reference to the rear pressure
dome, i.e. the dome of the rear pressure bulkhead, of an aircraft.

[0003]In the production of structural components in the aircraft sector,
on the one hand certain weight specifications have to be observed, but on
the other hand the production of such structural components must also be
economical. In the aerospace industry, composite materials are
increasingly replacing metal materials, since they are much lighter than
metal materials. Every kilogram of weight that is saved advantageously
reduces fuel costs or increases the payload.

[0004]For example, lightweight carbon-fibre reinforced plastics (CRP) are
used for the production of wing trusses, landing flaps, rear fuselage
sections with horizontal and vertical tail empennages and the
aforementioned pressure dome. For economic reasons, airliners fly at
altitudes of about 10 to 15 km. To be able to survive at these altitudes,
a pressurized cabin is required. In this, a pressure that corresponds to
a flying height of approximately 3 km is maintained. The pressure dome
forms the rear end part for this pressurized cabin. During the flight, it
bears the entire internal cabin pressure. Together with a ring of
titanium, for example, and numerous angles for introducing force into the
fuselage structure, the dome is mounted in a clamped manner on the
assigned ring in front of the vertical empennage.

[0005]For components of a large area and little curvature, such as for
example the empennage panels, at present resin-impregnated carbon fibre
strips (known as prepregs) are used. These are laboriously brought into
the later shape and cured by means of pressure and heat in what is known
as an autoclave.

[0006]However, the methods so far known to the applicant for the manual
laying of the prepreg strips are mainly suitable for geometries that are
simple and have little curvature. In the case of more complex geometries
to be laid, the laying rate is reduced to a value that is no longer
economical. Furthermore, the pre-impregnated prepreg strips are
relatively expensive and can only be stored under certain conditions.

[0007]For structures that have a greater curvature or are more complex,
the applicant has developed a novel production concept, which is
mentioned in the trade journal HIGH PERFORMANCE, Composites May 2003,
page 45 et seq.; the trade journal Forum, July 2004, page 8 et seq. and
in the trade journal Innovate!, "Flugzeugbau mit Nadel und Faden und
neuen Werkstoffen" [aircraft construction with needle and thread and new
materials), page 24 et seq. Resin-free carbon fibre fabrics are
accordingly brought into the desired shape in the dry state, the resin
only being subsequently worked into the fabric. Resin-free carbon fibre
fabrics can be handled much more easily than sticky prepreg strips.
Individual, multi-axial carbon-fibre nonwoven fabrics are sewn together
by means of an automated sewing method to form a so-called nonwoven
carpet. In this nonwoven carpet, the carbon fibres are arranged in the
longitudinal and transverse directions. The individual multi-axial
carbon-fibre nonwoven fabrics or semifinished fibrous sheets are
therefore joined together, for example by sewing, to form large-area,
planar nonwoven carpets, rolled up on rolls and unrolled over a shaping
element.

[0008]When using previous laying techniques and installations for laying
the sewn carpets made up of individual multi-axial nonwoven sheets, one
problem would be that undesired folds or waves would form, in particular
in the edge regions, when the nonwoven carpets are laid on highly curved
shaping elements. The formation of such folds makes it considerably more
difficult to place the finished structural components against assigned
mounting parts during final assembly.

SUMMARY OF THE INVENTION

[0009]It is ONR object of the present invention to provide an apparatus
and a method of the type mentioned at the beginning that prevent the
occurrence of draping during the laying of the nonwoven carpets and
ensure the production of a wave-free structural component.

[0010]The invention provides an apparatus with the features of Patent
Claim 1 and a method with the features of Patent Claim 14.

[0011]One idea on which the present invention is based is that manual
laying of the fibrous sheets or nonwoven carpets is replaced by an
automated unrolling method by means of a corresponding apparatus
controlled by a central control device. In this case, a predetermined
shaping element is provided, a fibrous sheet is laid in a defined manner
over or into the predetermined shaping element by means of a controllable
laying device; the predetermined shaping element and the laying device
are turned by means of a controllable turning device in relation to each
other by a predetermined turning angle; and a further fibrous sheet is
laid in a defined manner on top of the already laid fibrous sheet by
means of the controllable laying device.

[0012]Consequently, a number of fibrous sheets or nonwoven carpets can be
laid in an automated and defined manner one on top of the other with
predetermined directions of orientation in such a way that the formation
of folds or waves, in particular in the edge region of the structural
component, is advantageously prevented on account of the exact
controlling of the laying operation. Consequently, structural components
with any imaginable geometry, in particular also with highly curved
surfaces, can be produced by the novel laying method and the novel
apparatus. Moreover, on account of the automated laying, the laying rate
is advantageously increased and the times when the apparatus is busy are
reduced.

[0013]Advantageous refinements and improvements of the apparatus specified
in Patent Claim 1 and of the method specified in Patent Claim 14 can be
found in the subclaims.

[0014]According to a preferred development, the predetermined shaping
element has the form of the structural component to be produced, for
example in the case of a pressure dome to be produced the form of a
turned-out shallow dish with an oval or circular cross section. The
shaping element serves for the laying of the corresponding resin layer
and the individual fibrous sheet and predefines the form of the
structural component to be produced. The automated laying method and the
controllable laying device also allow quite highly curved shaping
elements to be covered with the corresponding fibrous sheets economically
and without the formation of folds.

[0015]According to a further preferred development, the laying device has
four lifting columns, which are arranged in pairs around the shaping
element and can be synchronously controlled by the central control
device. Each pair of lifting columns is preferably respectively assigned
a vertically adjustable cross member, which respectively comprise two
receiving carriages that can be displaced synchronously along the
respective cross member and are intended for receiving predetermined
fibrous sheet rolls. The receiving carriages on the one hand and the
cross members on the other hand are adjusted transversely and vertically
by the central control device in such a way that automated and defined
guiding of the fibrous sheet rolls over the shaping element is
accomplished, and consequently defined laying of the fibrous sheet on the
shaping element. The central control device activates the lifting columns
for a synchronous vertical adjustment of the assigned cross members along
the lifting columns and the receiving carriages for a synchronous
transverse adjustment of the receiving carriages, and consequently the
fibrous sheet rolls, along the cross members suitably in a predetermined
way.

[0016]Advantageously, two fibrous sheet rolls are guided uniformly and
synchronously from the centre of the predetermined shaping element to the
edge of the same by means of the laying device controlled by the central
control device, for uniform laying of the fibrous sheet over or into the
predetermined shaping element above the same. For this purpose,
synchronous controlling of the receiving carriages and of the lifting
columns is performed by the central control device.

[0017]Preferably a number of fibrous sheets, for example six, are laid one
on top of the other over or into the predetermined shaping element, the
central control device instigating that, after each laying of a fibrous
sheet, the predetermined shaping element is turned by means of the
turning device by a predetermined turning angle, for example 30°,
in relation to the laying device and is arrested. Consequently, a
predetermined rolling rate, a predetermined advancing rate and/or a
predetermined advancing amount of the fibrous sheet to be laid can be
advantageously controlled by the central control device during the laying
of the said sheet over or into the shaping element.

[0018]According to a further preferred exemplary embodiment, in the event
of a failure of the automatic controlling by means of the central control
device, the laying device is operated in emergency mode for manual laying
of the fibrous sheet. Consequently, a laying operation that has been
commenced can be manually completed, in order to prevent loss of the
component.

BRIEF DESCRIPTION OF THE DRAWINGS

[0019]The invention is explained in more detail below on the basis of
exemplary embodiments with reference to the accompanying figures of the
drawing, in which:

[0020]FIG. 1 shows a front view of an apparatus according to a preferred
exemplary embodiment of the present invention in a roll receiving state;

[0021]FIG. 2 shows a left-side view of the apparatus from FIG. 1, given by
way of example, in a first roll moving state;

[0022]FIG. 3 shows a front view of the apparatus from FIGS. 1 and 2, given
by way of example, in the roll receiving state and in the first roll
moving state;

[0023]FIG. 4 shows a left-side view of the apparatus from FIGS. 1 to 3,
given by way of example, in a second roll moving state;

[0024]FIG. 5 shows a left-side view of the apparatus from FIGS. 1 to 4,
given by way of example, in a third roll moving state; and

[0025]FIG. 6 shows a left-side view of an apparatus according to a further
preferred exemplary embodiment of the present invention.

[0026]Unless otherwise specified, in the figures the same reference
numerals designate components that are the same or functionally the same.

DETAILED DESCRIPTION OF THE INVENTION

[0027]In FIGS. 1 to 5, an apparatus for producing a structural component
from a fibre-composite material, for example a carbon-fibre reinforced
plastic (CRP), according to a preferred exemplary embodiment of the
present invention is represented. In this case, FIGS. 1 and 3 illustrate
a front-side view and FIGS. 2, 4 and 5 illustrate a left-side view of the
apparatus in different moving states.

[0028]The apparatus given by way of example preferably has a shaping
element 1, which is formed for example as a positive adhesive-bonding
device of structural steel or the like. The dimensions of the shaping
element 1 are adapted to the desired dimensions of the structural
component to be produced, for example the pressure dome to be produced.
Any different coefficients of thermal expansion of the moulding material
in comparison with the material of the component are preferably already
suitably compensated in the structural design of the shaping element 1.

[0029]For the production of a pressure dome for an aircraft, the shaping
element 1 is advantageously formed as a turned-out, shallow dish.
Depending on the type of aircraft, the shaping element 1 may have, for
example, an oval or circular cross-sectional form.

[0030]Preferably, prepreg doublers and/or edge reinforcing layers are
first applied to predetermined locations on the surface of the shaping
element 1, for example to reinforce cutouts or the like that are later to
be provided in the pressure dome. Segment doublers and edge reinforcing
layers comprise prepreg blanks and are supplied for example by means of
an ultrasonic cutter and positioned at the corresponding locations of the
shaping element. Subsequently, a suitable resin film is correspondingly
cut to size by means of templates and laid over the entire shaping
element 1.

[0031]Individual nonwoven sheets of preferably a carbon-fibre reinforced
plastic are joined together by a suitable joining method, for example
sewing, tacking, knitting, adhesive bonding or the like, to form a
large-area nonwoven carpet 15. By skilful thread guidance, it is possible
for example in a sewing process for each location of a component to be
adapted to the greatest extent to the loads that will later occur at this
location. The nonwoven sheets are preferably joined together without
previously being enveloped in synthetic resin. Resin-free carbon fibre
fabrics can be handled more easily than sticky prepregs.

[0032]By such a joining method, a large nonwoven carpet 15 is produced in
advance, for example from carbon fibre material in which the carbon
fibres are preferably arranged in the longitudinal and transverse
directions. In order to achieve a structurally adapted strength of the
carbon material, later a number of these nonwoven carpets 15, preferably
six, are laid one on top of the other in different directions, which is
explained in more detail further below.

[0033]The nonwoven carpets 15 are advantageously already in each case
prefabricated to the form of the structural component to be produced, in
order to minimize as much as possible the scrap produced. The
sewn-together nonwoven carpets 15 to be laid are in each case wound up
uniformly and symmetrically onto a roll system comprising preferably two
nonwoven rolls, so that in the wound-up state the axis of symmetry of the
nonwoven carpet 15 is preferably arranged between the two nonwoven rolls.
The nonwoven rolls are provided in the figures with the reference
numerals 2 and 3.

[0034]Subsequently, the nonwoven carpets 15 rolled up on the nonwoven
rolls are laid by means of an apparatus onto the assigned shaping element
1, which is explained in more detail below with reference to the figures.

[0035]As is further evident from FIGS. 1 to 5, apart from the shaping
element 1, the apparatus also has a laying device, which comprises a
lifting column system surrounding the shaping element 1 and preferably
comprising four lifting columns 4. On both sides of the shaping element
1, two lifting columns 4 for example are provided for respectively
forming a pair of lifting columns, as represented in particular in FIG.
2. The two pairs of lifting columns are preferably arranged symmetrically
in relation to each other and have in each case an assigned cross member
5.

[0036]Integrated in each cross member 5 are, for example, two
synchronously, electromotively driven receiving carriages 6, which are
displacably mounted so as to slide in the transverse direction along the
assigned cross member 5 by means of controlling by a central control
device. The cross members 5 are in turn preferably vertically adjustable
by the lifting columns 4, which can be synchronously controlled by the
central control device, so that the receiving carriages 6 can be
synchronously adjusted both in the transverse direction and in the
vertical direction by appropriate controllings.

[0037]The nonwoven rolls 2, 3 are preferably provided in the rolled-up
state in a suitable transporting car 8, which is positioned by means of
suitable positioning means 9 in relation to the receiving carriages 6, as
is evident for example in FIGS. 1 to 3.

[0038]According to the present exemplary embodiment, as is evident from
FIG. 1, the nonwoven rolls 2, 3 are received in a defined transfer
position directly from a transporting car 8 and made to move from the
receiving position represented in FIG. 1 into the position represented in
FIG. 2. For this purpose, the lifting columns 4 are controlled by means
of the central control device in such a way that the assigned cross
members are adjusted to a predetermined height after receiving the rolls.

[0039]Subsequently, the receiving carriages 6, which in each case have for
example electromotive drives which are connected to the central control
device for controlling of the same, are made to move by appropriate
controlling from the position represented in FIG. 2 along the cross
members 5 into the initial laying position according to FIG. 4. In this
initial laying position, the laying rolls 2, 3 are preferably over the
centre of the shaping element 1. Exact positioning of the nonwoven rolls
2, 3 or the nonwoven carpet 15 to be laid with respect to the shaping
element is accomplished for example by means of applied markings and/or
an additional positioning device, for example an optical positioning
device.

[0040]The overall sequence of movements of the nonwoven rolls 2, 3 is made
up of the vertical adjustment of the cross members 5 and the transverse
adjustment of the receiving carriages 6, the overall laying operation and
nonwoven roll guiding operation being accomplished under program control
by the central control device. The lifting columns 4 and the receiving
carriages 6 are preferably controlled in a synchronous and defined manner
by the central control device in such a way that the nonwoven carpet 15
rolled up on the nonwoven rolls 2, 3 is laid in an automated manner at a
predetermined, defined rolling rate, advancing rate and/or advancing
amount onto the shaping body 1.

[0041]Starting from the state represented in FIG. 4, for example, the two
nonwoven rolls 2, 3 are brought uniformly from the centre of the shaping
element 1 to the edge of the same, as schematically represented by the
states of the nonwoven rolls 2, 3 in FIGS. 4 and 5.

[0042]In order to avoid displacement of nonwoven carpets that have already
been applied, the nonwoven rolls 2, 3 are preferably guided in a
self-supporting manner approximately 50 mm above the shaping element 1.
Here, the roll drives of the nonwoven rolls 2, 3 advantageously do not
exert any additional forces on the nonwoven carpet 15. Suitable centring
pins 7 at the ends of the nonwoven rolls 2, 3 serve to ensure that they
are exactly received on the assigned receiving carriages 6 and that the
nonwoven rolls 2, 3 are exactly guided over the shaping element 1.

[0043]Such defined, automatic unrolling of the nonwoven carpet 15 to be
laid onto the shaping element 1 allows a high laying rate and fold-free
or wave-free laying to be achieved, even in the edge regions. This
automated laying operation also ensures a reproducible laying process, so
that even structural components with highly curved surfaces are
accomplished without the formation of folds, for good attachment to
assigned mounting parts.

[0044]The apparatus according to the present preferred exemplary
embodiment also has, furthermore, a turntable 10, on which the shaping
element 1 is mounted. The turntable 10 is preferably likewise connected
to the central control device for turning control of the same. Such a
turning movement is preferably accomplished by means of an electromotive
drive 11, which can be controlled by the central control device in a way
known per se. The turntable 10 also has, for example, a positioning
device 12, which serves for exactly positioning the turntable 10 by the
prescribed turning angle. Suitable controlling accordingly allows the
turntable 10 to move the shaping element 1 into any turned position.

[0045]Preferably, after laying a nonwoven carpet 15 onto the shaping
element 1 according to the method described above, the shaping element 1
is turned on the turntable 10 by means of the controlled electromotive
drive 11, by for example 30°, in relation to the lifting column
system and is suitably fixed.

[0046]Subsequently, a further nonwoven carpet 15 is laid on top of the
previously applied nonwoven carpet or carpets 15 in the manner described
above.

[0047]This operation can be repeated several times in succession in a
suitable way. In order to achieve a structurally adapted strength of the
fibre material, for example six nonwoven carpets 15 of this kind are laid
one on top of the other, turned by 30° in different directions. It
is obvious to a person skilled in the art that a number of nonwoven
carpets 15 other than six may be laid one on top of the other, the
turning angle of the turning device preferably being adapted
correspondingly to the number of nonwoven carpets 15 to be laid.

[0048]After applying all the nonwoven carpets 15 to the shaping element 1,
prepreg reinforcements such as those initially applied are in turn
applied, preferably symmetrically in relation to the latter, in the
predetermined regions of the shaping element 1.

[0049]Finally, the shaping element 1 together with the laid nonwoven
carpets 15 and reinforcements and/or applied stiffeners are introduced
into a suitable baking oven, known as an autoclave. There, the synthetic
resin, for example epoxy resin, laid as films, is pressed between the
individual nonwoven carpets 15 by a vacuum and is cured. In this way, the
desired structural component, for example a pressure dome for an
aircraft, is obtained after removal from the shaping element 1.

[0050]On account of the high degree of automation, the method described
above and the apparatus described are extremely economical and very
reliable. Suitable guidance control of the nonwoven rolls advantageously
allows damage to the fibres of the nonwoven carpets 15 to be avoided
during the laying operation.

[0051]The apparatus additionally has for example a positioning device,
which is formed for example as a linear laser projector. This positioning
device serves in particular for positioning the prepreg reinforcements to
be laid on the shaping element 1, or stiffeners to be additionally
applied, in conjunction with the defined turntable position.

[0052]All component parts of the installation that come into contact with
or reach over the nonwoven carpet 15 are advantageously designed in such
a way as to preclude soiling of the nonwoven carpet 15 and any not fully
cured stiffeners, for example by fluff, abrasive matter, oil or colour
particles. This applies in particular to all component parts of the
laying device 4, 5, 6 and of the podium described further below that do
not contain any lubricants such as oils, greases or silicone-containing
lubricating and sliding substances. All drive devices of the turntable 10
and of the entire laying device 4, 5, 6 are also preferably guarded with
sheet metal covers to prevent operating personnel reaching in. Moreover,
these covers guard the nonwoven carpets 15 against the escape of any
operating fluids or materials that may be present.

[0053]The apparatus explained in more detail above normally operates in
automatic mode, in which the central control device controls the guidance
of the nonwoven rolls for laying the nonwoven carpets 15 onto the shaping
element 1. In the event of failure of the automatic control or of certain
drive devices, an emergency mode is preferably provided, a mode in which
a laying operation that has been commenced can be manually completed, in
order to prevent loss of the structural component. In order to avoid or
eliminate risks for the operating personnel and damage in the apparatus,
an emergency-off device is preferably installed in compliance with safety
regulations.

[0054]FIG. 6 schematically illustrates a left-side view of an apparatus
for producing a large-area fibre-composite structural component according
to a further preferred exemplary embodiment of the present invention. As
is evident in FIG. 6, in addition to the component parts described above,
the apparatus has a movable podium 13, which is formed for example as a
staircase landing with foldable platforms 14. In FIG. 6, possible
adjusting and folding movements are schematically represented by the
indicated arrows. However, it is obvious to a person skilled in the art
that further refinements of the podium 13 are possible.

[0055]For example, the podium 13 is rail-guided, to allow the tilting
moment in a working position to be absorbed, the rail system
advantageously being sunk in the floor of the factory to avoid edges that
could be tripped over. The podium 13 may for example be made to move
manually or electronically by means of an assigned control device and be
arrested in the respective servicing and/or working position. As a
result, the shaping element 1 can be reached by the operating personnel
at any time and at any location.

[0056]Although the present invention has been described here on the basis
of preferred exemplary embodiments, it is not restricted to these but can
be modified in a wide variety of ways.

[0057]For example, the laying device may also comprise a square frame
which is mounted by means of a number of rollers on a ring rail. The ring
rail is provided for example with a number of bores, in order to fix the
frame in the respectively desired angle of orientation by stop pins. The
shaping element is fixedly mounted in the middle of the ring rail, which
is for example bolted to the floor, so that a relative turning of the
frame in relation to the shaping element is accomplished by turning the
square frame along the ring rail.

[0058]Preferably fastened on the rotatably mounted, square frame are two
arcuate running rails, on each of which two controllable carriages are
adjustably mounted. Rotatably mounted on each carriage is one end of the
nonwoven rolls. By suitable controlling of the carriages, the latter are
synchronously guided along the arcuate running rails, so that the
nonwoven rolls roll out, for example from the centre of the shaping
element over the shaping element to the edge of the same. The form of the
arcuate running rails is to be adapted here to the form of the shaping
element or the form of the structural component to be produced.